Aerodynamic Shape Optimization of Morphing Wings at Multiple Flight Conditions
Author:
Affiliation:
1. Utah State University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1420
Reference19 articles.
1. Lifting-Line Analysis of Roll Control and Variable Twist
2. Predicting Maximum Lift Coefficient for Twisted Wings Using Lifting-Line Theory
3. Fluid-Structure Interaction of a Variable Camber Compliant Wing
4. Investigation into the Effect of Shape Deviation on Variable Camber Compliant Wing Performance
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